Garmin G1000 - Diamond DA42NG User guide

Type
User guide

This manual is also suitable for

®
G1000
®
Pilot’s Guide
G1000
®
Integrated Flight Deck
Pilot’s Guide
Diamond DA42NG
Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
Tel: 913.397.8200
Fax: 913.397.8282
AOG Hotline: 913.397.0836
Aviation Dealer
Technical Support: 888.606.5482
www.garmin.com
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Tel: 503.581.8101
Fax: 503.364.2138
Garmin (Europe) Ltd.
Liberty House,Houndsdown Business Park
Southampton, Hampshire, SO40 9LR, U.K.
Tel: +44 (0) 238 052 4000
Fax: +44 (0) 238 052 4004
Aviation Support: +44 (0) 370 850 1243
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District,
New Taipei City, Taiwan
Tel: 34-93-357-2608
Fax: 34-93-429-4484
Diamond DA42NG
190-00962-04
Revision A
SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
EIS
AUDIO PANEL & CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AFCS
ADDITIONAL FEATURES
APPENDICES
INDEX
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
190-00962-04 Rev. A
Copyright © 2008, 2009, 2011, 2012, 2014 and 2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0752.13 or later for the Diamond DA42NG Some differences in operation
may be observed when comparing the information in this manual to earlier or later software versions.
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
Tel: 913.397.8200
Fax: 913.397.8282
Aircraft On Ground (AOG) Hotline: 913.397.0836
Aviation Dealer Technical Support: 888.606.5482
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Tel: 44.(0).23.8052.4000
Fax: 44.(0).23.8052.4004
Aviation Support: 44.(0).37.0850.1243
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Tel: 503.581.8101
Fax 503.364.2138
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District, New Taipei City, Taiwan
Tel: 34.93.357.2608
Fax: 34.93.429.4484
Website Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download
a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for
personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice
and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin
®
is a registered trademark of Garmin Ltd. or its subsidiaries, and G1000
®
is a trademark of Garmin Ltd. or its subsidiaries. These
trademarks may not be used without the express permission of Garmin.
Honeywell
®
is a registered trademark of Honeywell International, Inc. Stormscope
®
is a registered trademark of L-3 Communications.
Avidyne
®
is a registered trademark of Avidyne Corporation. AC-U-KWIK
®
is a registered trademark of Penton Business Media Inc. SiriusXM
Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively AOPA”) expressly disclaim all warranties,
with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties
of merchantability and fitness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any
representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any
incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if
AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to
the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual
or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for
incidental or consequential damages so the above limitations or exclusions may not apply to you.
AC-U-KWIK and its related organizations (hereafter collectively AC-U-KWIK Organizations”) expressly disclaim all warranties with
respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of
merchantability and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or
make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the
maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related
to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions
do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations
or exclusions may not apply to licensee.
May 2016 Printed in the U.S.A
190-00962-04 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
i
WARNINGS, CAUTIONS, AND NOTES
WARNING: Do not use terrain avoidance displays as the sole source of information for maintaining separation
from terrain and obstacles. Garmin obtains terrain and obstacle data from third party sources and cannot
independently verify the accuracy of the information.
WARNING: Always refer to current aeronautical charts and NOTAMs for verification of displayed aeronautical
information. Displayed aeronautical data may not incorporate the latest NOTAM information.
WARNING: Do not use geometric altitude for compliance with air traffic control altitude requirements. The
primary barometric altimeter must be used for compliance with all air traffic control altitude regulations,
requirements, instructions, and clearances.
WARNING: Do not use basemap information (land and water data) as the sole means of navigation. Basemap
data is intended only to supplement other approved navigation data sources and should be considered only
an aid to enhance situational awareness.
WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic
within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information
from aircraft or ground stations, traffic may be present that is not represented on the display.
WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous
weather. Information contained within data link weather products may not accurately depict current
weather conditions.
WARNING: Do not use the indicated data link weather product age to determine the age of the weather
information shown by the data link weather product. Due to time delays inherent in gathering and processing
weather data for data link transmission, the weather information shown by the data link weather product
may be significantly older than the indicated weather product age.
WARNING: The displayed minimum safe altitude (MSAs) are only advisory in nature and should not be relied
upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical
charts for appropriate minimum clearance altitudes.
WARNING: Always obtain qualified instruction prior to operational use of this equipment.
WARNING
:
Do not use a QFE altimeter setting with this system. System functions will not operate properly
with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the
standard pressure setting, as applicable.
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
190-00962-04 Rev. Aii
WARNINGS, CAUTIONS, AND NOTES
WARNING
:
Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a
system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that
may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned
in error as displayed.
WARNING: When using the autopilot to fly an approach with vertical guidance, the autopilot will not level
the aircraft at the MDA/DH even if the MDA/DH is set in the altitude preselect.
WARNING: Do not rely solely upon the display of traffic information for collision avoidance maneuvering.
The traffic display does not provide collision avoidance resolution advisories and does not under any
circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft.
WARNING
:
Because of variation in the earth’s magnetic field, do not rely on the accuracy of attitude and
heading indications (GRS 77 installations only) in the following geographic areas: North of 72° North
latitude at all longitudes; South of 70° South latitude at all longitudes; North of 65° North latitude between
longitude 75° W and 120° W. (Northern Canada); North of 70° North latitude between longitude 70° W and
128° W. (Northern Canada); North of 70° North latitude between longitude 85° E and 114° E. (Northern
Russia); South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and
New Zealand).
WARNING: Do not rely on information from a lightning detection system display as the sole basis for hazardous
weather avoidance. Range limitations and interference may cause the system to display inaccurate or
incomplete information. Refer to documentation from the lightning detection system manufacturer for
detailed information about the system.
WARNING:
Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance.
Garmin SVT is intended as an aid to situational awareness only and may not provide either the accuracy or
reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic.
WARNING:
Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may
appear as a partial symbol.
WARNING:
Do not use the Garmin SVT runway depiction as the sole means for determining the proximity of
the aircraft to the runway or for maintaining the proper approach path angle during landing.
WARNING: Do not operate the weather radar in a transmitting mode when personnel or objects are within
the MPEL boundary.
190-00962-04 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
iii
WARNINGS, CAUTIONS, AND NOTES
WARNING: Always position the weather radar gain setting to Calibrated for viewing the actual intensity of
precipitation. Changing the gain in weather mode causes precipitation intensity to be displayed as a color
not representative of the true intensity.
CAUTION: Do not clean display surfaces with abrasive cloths or cleaners containing ammonia. They will
harm the anti-reflective coating.
CAUTION:
Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or
modifications could void both the warranty and affect the airworthiness of the aircraft.
NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information.
Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control.
NOTE: All visual depictions contained within this document, including screen images of the system panel
and displays, are subject to change and may not reflect the most current system and aviation databases.
Depictions of equipment may differ slightly from the actual equipment.
NOTE: The United States government operates the Global Positioning System and is solely responsible for
its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and
performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation
AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or
misinterpreted and, therefore, become unsafe.
NOTE
: This device complies with part 15 of the FCC Rules. Operation is subject to the following two
conditions: (1) this device may not cause harmful interference, and (2) this device must accept any
interference received, including interference that may cause undesired operation.
NOTE
: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of
attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards
away from the source of the interference should alleviate the condition.
NOTE
: Use of polarized eyewear may cause the flight displays to appear dim or blank.
NOTE
: This product, its packaging, and its components contain chemicals known to the State of California
to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with
California’s Proposition 65. If you have any questions or would like additional information, please refer to
our web site at www.garmin.com/prop65.
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
190-00962-04 Rev. Aiv
WARNINGS, CAUTIONS, AND NOTES
NOTE: Operating the system in the vicinity of metal buildings, metal structures, or electromagnetic fields
can cause sensor differences that may result in nuisance miscompare annunciations during start up, shut
down, or while taxiing. If one or more of the sensed values are unavailable, the annunciation indicates no
comparison is possible.
NOTE: The system responds to a terminal procedure based on data coded within that procedure in the
Navigation Database. Differences in system operation may be observed among similar types of procedures
due to differences in the Navigation Database coding specific to each procedure.
NOTE
: The FAA has asked Garmin to remind pilots who fly with Garmin database-dependent avionics of the
following:
It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information
related to the use of databases in the National Airspace System.
• Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases
obtained from Garmin or Jeppesen are assured compliance with all data quality requirements (DQRs) by virtue
of a Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database
and can be viewed at http://fly.garmin.com by selecting ‘Type 2 LOA Status.
Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with
established FAA regulatory guidance, but does not constitute authorization to fly any and all terminal procedures
that may be presented by the system. It is the pilot’s responsibility to operate in accordance with established
AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment.
NOTE
: The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed in
SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at
www.flygarmin.com by selecting ‘Database Exclusions List.
NOTE
: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their
impact on the intended aircraft operation. The database alerts can be viewed at www.flygarmin.com by
selecting ‘Aviation Database Alerts.
NOTE
: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support to
coordinate the revised DQRs.
NOTE: Garmin requests the flight crew report any observed discrepancies related to database information.
These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles
and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go
to FlyGarmin.com and select Aviation Data Error Report’.
190-00962-04 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
v
WARNINGS, CAUTIONS, AND NOTES
NOTE: Lamp(s) inside this product contain mercury (HG) and must be recycled or disposed of according to
local, state, or federal laws. For more information, refer to our website at www.garmin.com/aboutGarmin/
environment/disposal.jsp
NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms
that can cause isolated discharge points in the strike display mode. However, clusters of two or more
discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after
the screen has been cleared.
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
190-00962-04 Rev. Avi
WARNINGS, CAUTIONS, AND NOTES
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190-00962-04 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
vii
REVISION INFORMATION
Record of Revision
Part Number Revision Date Page Range Description
190-00962-00 A 02/19/09 i – I-6 Initial release with GDU SW Version 9.05
190-00962-00 B 04/29/09 i – I-6 Added Synthetic Vision System
190-00962-01 A 03/14/11 i – I-6 Added GDU 11.12
Added Database Synchronization
Added Electronic Checklists
Added AOPA Airport Directory
Added flight plan import/export
Added Auxiliary Video
Changed procedure for creating user waypoints
190-00962-02 A 06/15/12 i – I-6 Added GDU 12.03
190-00962-02 B March
2014
All Added Underspeed Protection
Updated ESP pitch limits
Changed GFC 700 to Garmin AFCS
Added LP approaches
190-00962-03 A October
2014
All Updated System Message Advisories
Updated Weather Radar
Added Radar Altimeter
Updated EIS strip
Added ADS-B out capablility
Added other GDU 14.02 parameters
Changed GFDS to Connext
Changed Synthetic Vision System (SVS) to Synthetic Vision
Technology (SVT)
Added User Defined Holding Patterns
Added Temperature Compensated Altitude
Updated Warnings, Cautions, and Notes
190-00962-04 A May 2016 All Added Support for GDL 69/69A SXM
Added Support for ADS-B Traffic
Added Support for FIS-B Weather
Added Bluetooth
®
connectivity
Updated Warnings, Cautions, and Notes
Added other GDU 15.11 parameters
Added Support for GSR 56 Iridium Transceiver
Added Wi-Fi connectivity
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
190-00962-04 Rev. Aviii
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 Line Replaceable Units ........................................... 2
1.2 Secure Digital (SD) Cards .......................................6
1.3 System Power-up ..................................................... 7
1.4 System Operation .................................................... 8
Display Operation ......................................................... 8
G1000 System Annunciations ........................................ 9
System Status ............................................................. 11
AHRS Operation ......................................................... 13
GPS Receiver Operation .............................................. 14
1.5 G1000 Controls ...................................................... 18
PFD/MFD Controls ...................................................... 18
Softkey Function ......................................................... 20
1.6 Accessing G1000 Functionality............................ 27
Menus ....................................................................... 27
Data Entry.................................................................. 27
Page Groups .............................................................. 29
System Settings .......................................................... 34
Timers ....................................................................... 40
Electronic Checklists ................................................... 42
1.7 Display Backlighting ............................................. 45
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 50
Airspeed Indicator ...................................................... 50
Attitude Indicator ....................................................... 52
Altimeter ................................................................... 53
Vertical Speed Indicator (VSI) ....................................... 55
Vertical Deviation ....................................................... 56
Horizontal Situation Indicator (HSI) .............................. 57
Course Deviation Indicator (CDI) .................................. 62
2.2 Supplemental Flight Data .................................... 69
Outside Air Temperature .............................................. 69
Wind Data ................................................................. 71
Vertical Navigation (VNV) Indications ........................... 72
2.3 PFD Annunciations and Alerting Functions ........ 73
System Alerting .......................................................... 73
Marker Beacon Annunciations...................................... 74
Traffic Annunciation .................................................... 74
Altitude Alerting ......................................................... 75
Low Altitude Annunciation .......................................... 75
Minimum Descent Altitude/Decision Height Alerting ...... 76
Radar Altimeter .......................................................... 77
2.4 Abnormal Operations ........................................... 79
Abnormal GPS Conditions ........................................... 79
Unusual Attitudes ....................................................... 80
SECTION 3 ENGINE INDICATION SYSTEM (EIS)
3.1 Engine Display ....................................................... 84
3.2 System Display ...................................................... 86
3.3 Fuel Display ............................................................ 88
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ................................................................ 91
MFD/PFD Controls and Frequency Display ..................... 92
Audio Panel Controls .................................................. 94
4.2 COM Operation ...................................................... 96
COM Transceiver Selection and Activation ..................... 96
COM Transceiver Manual Tuning .................................. 97
Quick-tuning and Activating 121.500 MHz .................... 98
Auto-tuning the COM Frequency .................................. 99
Frequency Spacing .................................................... 103
Automatic Squelch .................................................... 104
Volume .................................................................... 104
4.3 NAV Operation ..................................................... 105
NAV Radio Selection and Activation ........................... 105
NAV Receiver Manual Tuning ..................................... 106
Auto-tuning a NAV Frequency from the MFD ............... 108
Marker Beacon Receiver ............................................ 113
ADF/DME Tuning ...................................................... 114
4.4 GTX 33 Mode S Transponder .............................. 118
Transponder Controls ................................................ 118
Transponder Mode Selection ...................................... 119
Entering a Transponder Code ..................................... 121
IDENT Function ........................................................ 122
ADS-B TX ................................................................. 123
Flight ID Reporting.................................................... 124
4.5 Additional Audio Panel Functions ..................... 125
Power-up ................................................................. 125
Mono/Stereo Headsets .............................................. 125
Speaker ................................................................... 125
Intercom .................................................................. 126
Clearance Recorder and Player ................................... 128
Split COM ................................................................ 129
Entertainment Inputs ................................................ 129
4.6 Audio Panel Preflight Procedure ....................... 130
190-00962-04 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
ix
TABLE OF CONTENTS
4.7 Abnormal Operation ........................................... 131
Stuck Microphone ..................................................... 131
COM Tuning Failure ................................................... 131
Audio Panel Fail-Safe Operation ................................. 131
Reversionary Mode ................................................... 131
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 133
Navigation Status Box ............................................... 134
5.2 Using Map Displays ............................................. 136
Map Orientation ....................................................... 136
Map Range .............................................................. 138
Map Panning ............................................................ 140
Measuring Bearing and Distance ................................ 145
Topography .............................................................. 146
Map Symbols ........................................................... 149
Airways ................................................................... 155
Track Vector ............................................................. 157
Wind Vector ............................................................. 158
Nav Range Ring........................................................ 159
Fuel Range Ring ....................................................... 160
Field of View (SVS) .................................................... 161
Selected Altitude Intercept Arc ................................... 162
5.3 Waypoints ............................................................. 163
Airports ................................................................... 164
Intersections ............................................................ 171
NDBs ....................................................................... 173
VORs ....................................................................... 175
VRPs ....................................................................... 177
User Waypoints ........................................................ 179
5.4 Airspaces .............................................................. 185
5.5 Direct-to-Navigation .......................................... 189
5.6 Flight Planning ..................................................... 194
Flight Plan Creation .................................................. 195
Adding Waypoints to an Existing Flight Plan ................ 202
Adding Airways to a Flight Plan ................................. 205
Adding Procedures to a Stored Flight Plan .................. 207
Flight Plan Storage ................................................... 214
Flight Plan Editing .................................................... 216
Along Track Offsets ................................................... 219
Parallel Track ............................................................ 221
Activating a Flight Plan Leg ....................................... 224
Inverting a Flight Plan ............................................... 225
Flight Plan Views ...................................................... 226
Closest Point of FPL .................................................. 228
User-Defined Holding Patterns ................................... 228
5.7 Vertical Navigation ............................................. 233
Altitude Constraints .................................................. 235
5.8 Procedures ...........................................................239
Departures ............................................................... 240
Arrivals ................................................................... 243
Approaches ............................................................. 246
5.9 Trip Planning ........................................................ 254
Trip Planning ............................................................ 254
5.10 RAIM Prediction................................................... 258
5.11 Navigating a Flight Plan ..................................... 261
5.12 Abnormal Operation ........................................... 289
SECTION 6 HAZARD AVOIDANCE
6.1 SiriusXM Weather ................................................ 292
Activating Services .................................................... 292
Using SiriusXM Weather Products .............................. 293
6.2 Garmin Connext Weather ................................... 326
Registering the Iridium Satellite System ...................... 326
Registering Garmin Connext Weather ......................... 327
Accessing Garmin Connext Weather Products .............. 329
Connext Data Requests ............................................. 336
Garmin Connext Weather Products ............................. 340
Abnormal Operations ................................................ 355
6.3 FIS-B Weather ...................................................... 357
Using FIS-B Weather Products .................................... 357
FIS-B Weather Status................................................. 379
6.4 Airborne Color Weather Radar .......................... 380
System Description ................................................... 380
Principles of Pulsed Airborne Weather Radar ............... 380
Safe Operating Distance ............................................ 384
Basic Antenna Tilt Setup ............................................ 385
Weather Mapping and Interpretation ......................... 386
Ground Mapping and Interpretation ........................... 396
Weather Radar Overlay on the Navigation Map Page ... 397
System Status ........................................................... 399
6.5 WX-500 Stormscope ........................................... 401
Setting Up Stormscope on the Navigation Map ........... 401
Selecting the Stormscope Page .................................. 405
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
190-00962-04 Rev. Ax
TABLE OF CONTENTS
6.6 Terrain Proximity ................................................. 406
Displaying Terrain Proximity Data ............................... 406
Terrain Proximity Page ............................................... 409
6.7 Profile View Terrain ............................................. 411
Profile View Display .................................................. 412
6.8 Terrain-SVS ........................................................... 415
Displaying Terrain-SVS Data ....................................... 416
Terrain-SVS Page ...................................................... 418
Terrain-SVS Alerts ..................................................... 420
System Status ........................................................... 423
6.9 Traffic Information Service (TIS) ........................ 424
Displaying Traffic Data .............................................. 425
Traffic Map Page ....................................................... 427
TIS Alerts ................................................................. 428
System Status ........................................................... 429
6.10 Avidyne TAS600 Traffic ........................................ 432
TAS Symbology ......................................................... 432
Displaying Traffic Data .............................................. 433
Altitude Display ........................................................ 435
Traffic Map Page Display Range ................................. 435
TAS Alerts ................................................................ 437
System Status ........................................................... 438
6.11 Garmin GDL 88 ADS-B Traffic ............................. 439
ADS-B System Overview ............................................ 439
ADS-B with TAS ........................................................ 441
Conflict Situational Awareness & Alerting ................... 441
Airborne and Surface Applications .............................. 444
Traffic Description ..................................................... 445
Operation ................................................................ 445
System Status ........................................................... 454
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 458
7.2 Flight Director Operation ................................... 460
Activating the Flight Director ..................................... 460
AFCS Status Box ....................................................... 461
Command Bars ......................................................... 462
Flight Director Modes ................................................ 462
7.3 Vertical Modes ..................................................... 463
Pitch Hold Mode (PIT) ............................................... 464
Selected Altitude Capture Mode (ALTS) ....................... 465
Altitude Hold Mode (ALT) .......................................... 466
Vertical Speed Mode (VS) .......................................... 467
Flight Level Change Mode (FLC) ................................. 468
Vertical Navigation Modes (VPTH, ALTV) ..................... 469
Glidepath Mode (GP) (SBAS only) ............................... 474
Glideslope Mode (GS) ............................................... 476
Go Around Mode (GA) .............................................. 477
7.4 Lateral Modes ...................................................... 478
Roll Hold Mode (ROL) ............................................... 479
Heading Select Mode (HDG) ...................................... 480
Navigation Modes (GPS, VOR, LOC, BC) ...................... 481
Approach Modes (GPS, VAPP, LOC) ............................. 483
7.5 Autopilot and Yaw Damper Operation ............. 485
Flight Control ........................................................... 485
Engaging the Autopilot and Yaw Damper .................... 486
Control Wheel Steering ............................................. 486
Disengaging the Autopilot and Yaw Damper ................ 487
7.6 Example Flight Plan ............................................ 488
Departure ................................................................ 488
Intercepting a VOR Radial .......................................... 490
Flying a Flight Plan/GPS Course ................................. 491
Descent ................................................................... 492
Approach ................................................................. 495
Go Around/Missed Approach ..................................... 498
7.7 AFCS Annunciations and Alerts ......................... 500
AFCS Status Alerts .................................................... 500
Overspeed Protection ................................................ 501
Underspeed Protection .............................................. 501
Annunciations for KAP 140 Autopilot System .............. 503
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision Technology (SVT) ..................... 507
SVT Operation .......................................................... 508
SVT Features ............................................................ 510
Field of View ............................................................ 519
8.2 SafeTaxi ................................................................ 521
8.3 ChartView ............................................................. 527
ChartView Softkeys ................................................... 528
Terminal Procedures Charts ....................................... 529
Chart Options ........................................................... 537
Day/Night View ........................................................ 543
ChartView Cycle Number and Expiration Date ............. 546
8.4 FliteCharts ............................................................ 549
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TABLE OF CONTENTS
FliteCharts Softkeys .................................................. 550
Terminal Procedures Charts ....................................... 551
Chart Options ........................................................... 558
Day/Night View ........................................................ 562
FliteCharts Cycle Number and Expiration Date ............. 564
8.5 Airport Directory ................................................. 569
Airport Directory Database Cycle Number and Revision 569
8.6 SiriusXM Satellite Radio Entertainment ........... 573
Activating SiriusXM Satellite Radio Services ................ 573
Using SiriusXM Radio ................................................ 575
8.7 Satellite Telephone Services .............................. 579
Telephone Communication ........................................ 579
Text Messaging (SMS) ............................................... 586
8.8 Electronic Stability and Protection (ESP
) ....... 599
Roll Engagement ...................................................... 600
Pitch Engagement..................................................... 601
High Airspeed Protection ........................................... 602
8.9 Scheduler .............................................................. 603
8.10 Electronic Checklists ........................................... 605
8.11 Flight Data Logging ............................................ 609
8.12 Auxiliary Video ..................................................... 611
Video Setup .............................................................612
Display Selection ...................................................... 612
Zoom/Range ............................................................ 614
8.13 WI-FI Connections ............................................... 615
8.14 Abnormal Operation ........................................... 621
SVT Troubleshooting ................................................. 621
Reversionary Mode ................................................... 621
Unusual Attitudes ..................................................... 622
GDL 69/69A Data Link Receiver Troubleshooting .......... 622
APPENDICES
Annunciations and Alerts ............................................. 625
Flight Plan Import/Export Messages ........................... 645
TAS Alerts and Annunciations .................................... 647
TIS Alerts and Annunciations...................................... 648
SVS Terrain Alerts ...................................................... 649
SVS Terrain Status Annunciations ............................... 649
ADS-B Alerts and Annunciations ................................. 650
Weather Radar Alerts and Annunciations .................... 651
GDL 69A/GDL 69A SXM Data Link Receiver Messages .. 652
Database Management ............................................. 653
Navigation Databases ............................................... 653
Garmin Databases/Jeppesen Chartview Database ........ 658
Magnetic Field Variation Database Update .................. 664
Garmin Aviation Glossary ............................................ 665
Frequently Asked Questions ........................................ 674
General TIS Information ............................................... 678
Introduction ............................................................. 678
TIS VS. TAS/TCAS ....................................................... 678
TIS Limitations.......................................................... 678
Map Symbols ................................................................. 680
Telephone/Text Messaging ......................................... 684
INDEX
Index ................................................................................ I-1
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
190-00962-04 Rev. Axii
TABLE OF CONTENTS
Blank Page
190-00962-04 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
1
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
SECTION 1 SYSTEM OVERVIEW
NOTE: Refer to the Automatic Flight Control System (AFCS) Section for details on the Garmin AFCS.
The G1000 Integrated Flight Deck System presents flight instrumentation, position, navigation, communication,
and identification information using flat-panel color displays. The system is distributed across the following Line
Replaceable Units (LRUs):
GDU 1040
Primary Flight Display (PFD)
GDU 1045
Multi Function Display (MFD)
GMA 1347
Audio Panel with Integrated Marker
Beacon Receiver
GIA 63W
Integrated Avionics Units (IAU)
GDC 74A
Air Data Computer (ADC)
GEA 71
Engine/Airframe Unit
GTX 33 ES
Extended Squitter Mode S Transponder
GRS 77
Attitude and Heading Reference System
(AHRS)
GMU 44
Magnetometer
GDL 69/69A
or
69/69A SXM
Data Link Receiver
GSA 80
AFCS Yaw Damper Servo
GSA 81
AFCS Servos (3)
GSM 85 (
or
GSM 86)
Servo Mounts (4)
GSR 56
Iridium Transceiver
GWX 68/70
Weather Radar
GRA 5500
Radar Altimeter
Flight Stream 210
Wireless Bluetooth
®
Gateway
GDL 88
ADS-B Transceiver
GDL 59
Data Link
Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are shown in Figure 1-2.
The Diamond DA42NG may be optionally equipped with a Garmin AFCS Automated Flight Control System,
providing flight director (FD), autopilot (AP), and manual electric trim (MET) functions of the G1000 System.
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
190-00962-04 Rev. A2
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
1.1 LINE REPLACEABLE UNITS
GDU 1040/1045 (2) – A GDU 1040 is configured as the Primary Flight Display (PFD) and a GDU 1045 as
the Multi Function Display (MFD). Both displays feature 10.4-inch LCD screens with 1024 x 768 resolution.
The displays communicate with each other through a High-speed Data Bus (HSDB) Ethernet connection. Each
display is also paired with an Ethernet connection to an IAU.
GMA 1347
– The Audio Panel integrates navigation/communication radio (NAV/COM) digital audio, intercom,
and marker beacon controls, and is installed between the displays. This unit also provides manual control
of display Reversionary Mode (red
DISPLAY BACKUP
button; see Section 1.4, System Operation) and
communicates with both IAUs using an RS-232 digital interface.
GIA 63W
(2) – The Integrated Avionics Units (IAU) function as the main communications hub, linking all LRUs
with the PFD. Each GIA 63W contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, a flight director (FD;
if Garmin AFCS is installed), and system integration microprocessors. Each GIA 63W is paired with the on-side
display via an HSDB connection. The IAUs are not paired together and do not communicate with each other
directly.
NOTE: Refer to the Airplane Flight Manual (AFM) to determine whether SBAS functionality is approved.
GDC 74A
– The Air Data Computer (ADC) processes data from the pitot/static system and outside air temperature
(OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information to the G1000
System, and it communicates with the primary IAU, displays, and AHRS using an ARINC 429 digital interface.
GEA 71
– The Engine Airframe Unit receives and processes signals from the engine and airframe sensors. This
unit communicates with both IAUs using an RS-485 digital interface.
GTX 33 or GTX 33 with Extended Squitter
– The GTX 33 solid-state Transponder provides Modes A, C, and
S capability. The GTX 33 with Extended Squitter will also provide 1090 MHz Extended Squitter (1090ES)
transmit capability. The transponder communicates with both IAUs through an RS-232 digital interface.
GRS 77
(2) – The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading
information via ARINC 429 to both the PFD and the primary IAU. The AHRS contains advanced sensors
(including accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic field
information, with the ADC to obtain air data, and with both IAUs to obtain GPS information. AHRS operation
is discussed in Section 1.4, System Operation.
GMU 44
– The Magnetometer measures local magnetic field and sends data to the AHRS for processing to
determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates with
it via an RS-485 digital interface.
GDL 69/69A
or
69/69A SXM
– The Data Link Satellite Radio Receiver provides real-time weather information to
MFD maps and the PFD Inset Map. The GDL 69A model is also capable of providing digital audio entertainment.
The Data Link Receiver communicates with the MFD via an HSDB connection. A subscription to XM Satellite
Radio Service is required to enable Data Link Receiver capability.
GSA 80, GSA 81
and
GSM 85 (
or
GSM 86)
– The GSA servos are used for the automatic control of pitch, pitch
trim, roll and yaw. These units interface with each IAU.
The GSM 85 (or GSM 86) servo mounts are responsible for transferring the output torque of the servo actuators
to the mechanical flight-control surface linkages (not displayed in Figure 1-1).
190-00962-04 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
3
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
GRA 5500 (optional)
– The Radar Altimeter provides altitude above the ground (AGL) to the MFD, through the
GIA 63W, using an RS-422 digital interface.
GWX 68/70
– Provides airborne weather and ground mapped radar data to the MFD, via HSDB ethernet
connection.
GDL 88
(optional) – Provides ADS-B Traffic in and FIS-B Weather.
Flight Stream 210
(optional) – Provides wireless Bluetooth connectivity between a compatible tablet/mobile
device and the avionics system.
GDL 59
(optional) – Provides Wi-Fi capability
GSR 56
(optional) – The Iridium Transceiver provides voice communication by means of pilot and copilot
headsets. The unit can also send and receive data over the Iridium satellite network.
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
190-00962-04 Rev. A4
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
Figure 1-1 G1000 System Block Diagram
GMU 44
Magnetometer
Heading
Reversionary
Control
Reversionary
Control
GMA 1347
Audio Panel
GDU 1040
Primary Flight Display
GDU 1045
Multi Function Display
GDC 74A
Air Data
Computer
OAT
Airspeed
Altitude
Vertical Speed
GRS 77
AHRS
Attitude
Rate of Tu rn
Slip/Skid
GTX 33/33ES
Transponder
GEA 71
Engine/Airframe
Unit
GSA 81
Roll Servo
Autopilot Calculations
(optional)
GSA 81
Pitch Servo
Autopilot Calculations
(optional)
GSA 80
Ya w Damper Servo
Ya w Damper Calculations
(optional)
GSA 81
Pitch Tr im Servo
Autopilot Calculations
(optional)
No. 1 GIA 63W
Integrated Avionics Unit
System Inegration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/SBAS
Glideslope
Flight Director (with AFCS option)
GPS Output
No. 2 GIA 63W
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/SBAS
Glideslope
GPS Output
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Garmin G1000 - Diamond DA42NG User guide

Type
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